- #1
kepler
- 29
- 0
Hi,
since the previous conversion I needed doesn't seem to be of the common sense, let's try this: I have the orbital elements of a body referred to the equinox J2000 and to the equatorial plane. I need to transform the argument of the Perihélion, the inclination and the ascending node to the ecliptic plane and apply the precession to another epoch.
Any ideas?
Kepler
since the previous conversion I needed doesn't seem to be of the common sense, let's try this: I have the orbital elements of a body referred to the equinox J2000 and to the equatorial plane. I need to transform the argument of the Perihélion, the inclination and the ascending node to the ecliptic plane and apply the precession to another epoch.
Any ideas?
Kepler